|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-009/00 B64C-021/10 B64C-003/38 A63H-027/00 B64C-003/10 B64C-023/00 B64C-033/02 F01D-005/12|
|§371/§102 date||20121210 (20121210)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 2|
The invention relates to a wing for generating lift and comprises a trailing edge, a leading edge, an inner end, an outer end, a top surface and a bottom surface. The wing comprises an aerofoil with a chord line and a span direction. The leading edge comprises a kink between the inner end and the outer end. The leading edge comprises a forward sweep part between the inner end and the kink extending towards the kink presenting an angle relative to the span direction. The leading edge comprises a backward sweep part between the kink and the outer end exten...
1. A wing for generating lift from an incident flow comprising; a trailing edge, a leading edge, an inner end, an outer end, a top surface corresponding with a suction side and a bottom surface corresponding with a pressure side;in cross section, an aerofoil with a chord line which is defined by a straight line between the leading edge and the trailing edge of the aerofoil;a span direction that extends from the inner end towards the outer end which is perpendicular to the chord line;wherein the leading edge further comprises;a kink between the inner end ...